Incompressible flow over multi wing

CL, CD at different AoA, Pressure Graph and Aerodynamics efficiency.
At forward inclination 1-5 degree & same for backward.

Hi there, this is Fillia. If you need help with a project, please also share the link and more details :slight_smile:

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Fillia

Yes, Am trying to perform analysis of Multiplane. where i need to find out CL & CD at different AoA, Pressure Graph and Aerodynamics Efficiency also. where AoA is varying from 1-5 degree forward and backward.

Alright, then have a look at the following tutorials and pages:

You can use your own model for the simulation by following this CAD preparation& Upload guide:

Cheers!